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NASA Technical Reports Server (NTRS) 19940020019: NASA/USRA advanced design program

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NASA Technical Reports Server (NTRS) 19940020019: NASA/USRA advanced design program

by
NASA Technical Reports Server (NTRS)

Publication date
Topics
NASA Technical Reports Server (NTRS), AERODYNAMIC CHARACTERISTICS, AIRCRAFT DESIGN, HYPERSONIC AIRCRAFT, HYPERSONIC FLIGHT, HYPERSONICS, SUPERSONIC COMBUSTION RAMJET ENGINES, THERMAL PROTECTION, TRAJECTORY ANALYSIS, WEIGHT ANALYSIS, BOOSTER ROCKET ENGINES, COMPUTATIONAL FLUID DYNAMICS, COST ANALYSIS, FLIGHT CHARACTERISTICS, LIFTING BODIES, TEST VEHICLES,
Collection
NASA_NTRS_Archive; additional_collections
Language
English
This report analyzes and presents a preliminary design for an experimental hypersonic vehicle. This plane will have a cruise speed of Mach 12 for one minute at an altitude of 120,000 feet. The major design areas of aerodynamics, propulsion, and weights are discussed in depth. An elementary analysis of thermal protection, trajectory, and cost is also presented. Finally, a discussion of future plans and recommendations is given, and overall conclusions are drawn.
Addeddate
2016-10-01 05:39:04
Identifier
NASA_NTRS_Archive_19940020019
Identifier-ark
ark:/13960/t1sf7pk07
Ocr
ABBYY FineReader 11.0
Pages
79
Ppi
600
Year
1992

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